Doç. Dr. HARİKA SENEM KAHVECİ

Yayın Ağı

SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

Experimental investigation of momentum ratio and impingement angle effects on spray characteristics of triplet and pentad injectors

Gulmez S., Kahveci H. S.

International Journal of Multiphase Flow , cilt.177, 2024 (SCI-Expanded)

Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

Kahveci H. S.

Journal of Turbomachinery , cilt.143, sa.7, 2021 (SCI-Expanded)

Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer

Sakaoglu S., Kahveci H. S.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.142, sa.2, 2020 (SCI-Expanded)

Effect of turbulence modeling for the prediction of flow and heat transfer in rotorcraft avionics bay

Akin A., Kahveci H. S.

AEROSPACE SCIENCE AND TECHNOLOGY , cilt.95, 2019 (SCI-Expanded)

Effect of cavity depth on thermal performance of a cooled blade tip under rotation

Sakaoglu S., Kahveci H. S.

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER , cilt.143, 2019 (SCI-Expanded)

An optimization study for rotorcraft avionics bay cooling

Akin A., Kahveci H. S.

AEROSPACE SCIENCE AND TECHNOLOGY , cilt.90, ss.1-11, 2019 (SCI-Expanded)

EFFECTS OF PIN FIN SHAPE AND SIZE ON TURBINE BLADE TRAILING EDGE FLOW AND HEAT TRANSFER

Tuncel T., Kahveci H. S.

ISI BILIMI VE TEKNIGI DERGISI-JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY , cilt.39, sa.2, ss.191-207, 2019 (SCI-Expanded)

Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine

Kahveci H. S., Kırtley K.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.136, 2014 (SCI-Expanded)

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.135, 2013 (SCI-Expanded)

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.135, 2013 (SCI-Expanded)

Validation of MISES Two-Dimensional Boundary Layer Code for High-Pressure Turbine Aerodynamic Design

Andrew P., Kahveci H. S.

JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME , cilt.131, 2009 (SCI-Expanded)

Diğer Dergilerde Yayınlanan Makaleler

USE OF ARTIFICIAL NEURAL NETWORK IN ROTORCRAFT COOLING SYSTEM

Akin A., Kahveci H. S.

Havacılık ve Uzay Teknolojileri Dergisi , cilt.12, sa.2, ss.157-170, 2019 (Hakemli Dergi)

Hakemli Kongre / Sempozyum Bildiri Kitaplarında Yer Alan Yayınlar

Estimating Sweet Spot for UAV Formation Flight Using Vortex Lattice Method and Machine Learning

Tatar U., Kahveci H. S.

12th Ankara International Aerospace Conference (AIAC), Online, 13 - 14 Eylül 2023

Numerical Simulation of Spray Characteristics of Doublet Injectors

Gulmez S., Kahveci H. S.

11th Ankara International Aerospace Conference (AIAC), Virtual, Online, 8 - 10 Eylül 2021

Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

Kahveci H. S.

ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020, Virtual, Online, 21 - 25 Eylül 2020, cilt.7B-2020

Gas Turbine Blade Cooling Technology, Advances, and Challenges

Kahveci H. S.

10th Ankara International Aerospace Conference, Ankara, Türkiye, 18 - 20 Eylül 2019

EFFECT OF TURBINE BLADE TIP COOLING CONFIGURATION ON TIP LEAKAGE FLOW AND HEAT TRANSFER

Sakaoğlu S., Kahveci H. S.

ASME Turbo Expo: Turbomachinery Technical Conference and Exposition, Arizona, Amerika Birleşik Devletleri, 17 - 21 Haziran 2019

Comparison of Temperature Profile and Heat Transfer Predictions With Statistically Modeled Data From a Cooled 1 1 2 Stage High Pressure Transonic Turbine

Kahveci H. S., Kırtley K.

ASME Turbo Expo 2013, Volume 3C: Heat Transfer, Texas, Amerika Birleşik Devletleri, 3 - 07 Haziran 2013

Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part I Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B, Vancouver, Kanada, 6 - 10 Haziran 2011, cilt.5, ss.1719-1733

Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part II Effect of Cooling Variation on the Vane Airfoil and Inner Endwall

Kahveci H. S., Haldeman C., Mathıson R., Dunn M.

ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B, Vancouver, Kanada, 6 - 10 Haziran 2011, cilt.5, ss.1735-1744

Metrikler

Yayın

Atıf (WoS)

H-İndeks (WoS)

Atıf (Scopus)

130

Doç. Dr. HARİKA SENEM KAHVECİ

Yayınlar & Eserler

SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

Experimental investigation of momentum ratio and impingement angle effects on spray characteristics of triplet and pentad injectors

Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

Effect of Turbine Blade Tip Cooling Configuration on Tip Leakage Flow and Heat Transfer

Effect of turbulence modeling for the prediction of flow and heat transfer in rotorcraft avionics bay

Effect of cavity depth on thermal performance of a cooled blade tip under rotation

An optimization study for rotorcraft avionics bay cooling

EFFECTS OF PIN FIN SHAPE AND SIZE ON TURBINE BLADE TRAILING EDGE FLOW AND HEAT TRANSFER

Uncertainty Analysis of Heat Transfer Predictions Using Statistically Modeled Data From a Cooled 1-1/2 Stage High-Pressure Transonic Turbine

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall

Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine-Part I: Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Validation of MISES Two-Dimensional Boundary Layer Code for High-Pressure Turbine Aerodynamic Design

Diğer Dergilerde Yayınlanan Makaleler

USE OF ARTIFICIAL NEURAL NETWORK IN ROTORCRAFT COOLING SYSTEM

Hakemli Kongre / Sempozyum Bildiri Kitaplarında Yer Alan Yayınlar

Estimating Sweet Spot for UAV Formation Flight Using Vortex Lattice Method and Machine Learning

Numerical Simulation of Spray Characteristics of Doublet Injectors

Investigation of a rotor blade with tip cooling subject to a nonuniform temperature profile

Gas Turbine Blade Cooling Technology, Advances, and Challenges

EFFECT OF TURBINE BLADE TIP COOLING CONFIGURATION ON TIP LEAKAGE FLOW AND HEAT TRANSFER

Comparison of Temperature Profile and Heat Transfer Predictions With Statistically Modeled Data From a Cooled 1 1 2 Stage High Pressure Transonic Turbine

Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part I Experimental Configuration and Data Review With Inlet Temperature Profile Effects

Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part II Effect of Cooling Variation on the Vane Airfoil and Inner Endwall

Validation of MISES 2 D Boundary Layer Code for High Pressure Turbine Aerodynamic Design

Flow Around Helicopter Blade Tip Sections Using a 3D Stereoscopic Particle Image Velocimeter Part II

Flow Around Helicopter Blade Tip Sections Using a 2D Particle Image Velocimeter Part I

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Atıf (Scopus)

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